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Finite time oriented team forming air vehicle cooperative control method and control system

A time-limited, collaborative control technique used in the field of control science

Inactive Publication Date: 2018-03-27
西安恒律模训科技发展有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

On the other hand, in the actual control process, the formation system is often affected by constraints such as system nonlinearity, non-matching uncertainty, and directed communication, which brings great challenges to the design and stability analysis of formation finite-time control protocols. challenge

Method used

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  • Finite time oriented team forming air vehicle cooperative control method and control system
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  • Finite time oriented team forming air vehicle cooperative control method and control system

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Embodiment Construction

[0109] In order to understand the above-mentioned purpose, features and advantages of the present invention more clearly, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. It should be noted that, in the case of no conflict, the embodiments of the present application and the features in the embodiments can be combined with each other.

[0110] In the following description, many specific details are set forth in order to fully understand the present invention. However, the present invention can also be implemented in other ways different from those described here. Therefore, the protection scope of the present invention is not limited by the specific details disclosed below. EXAMPLE LIMITATIONS.

[0111] Such as figure 1 As shown, a schematic flow chart of a method for cooperative control of formation aircraft oriented to limited time according to an embodiment of the present invention. Amon...

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Abstract

The invention provides a finite time oriented team forming air vehicle cooperative control method and control system. The cooperative control method includes that a navigator and n followers form a team forming system and a dynamical model of the team forming system is established; measuring states of the team forming members; designing an ESO (Expansion State Observer) and an output value; basedon output of the ESO and the states of adjacent team forming members, calculating an integral type sliding mode variable structure of an i team forming member; based on the integral type sliding mode variable structure, designing a control protocol of the i team forming member so as to realize finite time coordination of the team forming state. According to the technical scheme provided bythe invention, aiming at influences due to constraints such as non-linear items, non-matching uncertainty, directional communication and the like in a practical team forming system, based on distributive control and a finite time control theory, based on the states of the adjacent team forming members, the ESO and the sliding mode control protocol are designed separately so as to ensure that theteam forming member state converges to the neighborhood of the navigator state in finite time.

Description

technical field [0001] The present invention relates to the field of control science and technology, in particular, to a limited-time-oriented cooperative control method for formation aircraft, a limited-time-oriented formation aircraft cooperative control system, a computer device, and a computer-readable storage medium. Background technique [0002] In recent years, spacecraft formations such as small satellites have attracted great attention from experts and scholars at home and abroad due to their huge advantages and broad prospects in the fields of military reconnaissance, deep space exploration, environmental monitoring, and positioning services. research direction. For formation vehicles, convergence performance / time is a key index and an important content in the field of cooperative control. For example, in practical applications, aerospace vehicles, multi-robot systems, etc. all require the control process to end within a limited time. In addition, in many industr...

Claims

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Application Information

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IPC IPC(8): G05D1/10
CPCG05D1/104
Inventor 马肸王业全武健孙明月
Owner 西安恒律模训科技发展有限公司
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